@inproceedings{oai:jaxa.repo.nii.ac.jp:00007689,
 author = {林, 一樹 and 土屋, 和雄 and Hayashi, Kazuki and Tsuchiya, Kazuo},
 book = {平成16年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers},
 month = {Mar},
 note = {地球周回軌道上の衛星(ターゲット)に対するサービスの1つとして操作可能な宇宙ロボット(チェイサ)がターゲットに接近し、外観の観察や修理などを行なうことが考えられている。本論文では非協力なターゲットに対するランデブ軌道制御の方法を提案する。提案する制御方法は、長楕円軌道上での運動解析をもとに周期的な状態遷移則を求めて、できるだけ簡単で最適な軌道制御が実現できるようにした。, This paper presents considerations of formulation and design for spacecraft rendezvous control on elliptic orbits around the earth. Spacecraft rendezvous is a key technique for orbital services to the target spacecraft such as resupply, review, assembling or mend. In order to formulate, it is needed to derive a linearized equation of relative motion between two spacecrafts (target and chaser) on an elliptic orbit. The solution of this equation is generally composed of periodic term and secular term (which is called drift motion in this paper). Based on this fact, a discrete state transition law of relative motion can be obtained, which enables realization of simple rendezvous control of the chaser., 資料番号: AA0047897056},
 pages = {324--329},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {A new approach for spacecraft rendezvous control on elliptic orbits},
 year = {2005}
}